DE60201325T2 - Hochdruck-Turbinenschaufel mit gekühlter Abströmkante - Google Patents

Hochdruck-Turbinenschaufel mit gekühlter Abströmkante Download PDF

Info

Publication number
DE60201325T2
DE60201325T2 DE60201325T DE60201325T DE60201325T2 DE 60201325 T2 DE60201325 T2 DE 60201325T2 DE 60201325 T DE60201325 T DE 60201325T DE 60201325 T DE60201325 T DE 60201325T DE 60201325 T2 DE60201325 T2 DE 60201325T2
Authority
DE
Germany
Prior art keywords
blade
foot
slot
closest
pressure turbine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE60201325T
Other languages
German (de)
English (en)
Other versions
DE60201325D1 (de
Inventor
Christian Bariaud
Jacques Boury
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA Moteurs SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Application granted granted Critical
Publication of DE60201325D1 publication Critical patent/DE60201325D1/de
Publication of DE60201325T2 publication Critical patent/DE60201325T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60201325T 2001-12-10 2002-12-03 Hochdruck-Turbinenschaufel mit gekühlter Abströmkante Expired - Lifetime DE60201325T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0115904A FR2833298B1 (fr) 2001-12-10 2001-12-10 Perfectionnements apportes au comportement thermique du bord de fuite d'une aube de turbine haute-pression
FR0115904 2001-12-10

Publications (2)

Publication Number Publication Date
DE60201325D1 DE60201325D1 (de) 2004-10-28
DE60201325T2 true DE60201325T2 (de) 2005-03-17

Family

ID=8870271

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60201325T Expired - Lifetime DE60201325T2 (de) 2001-12-10 2002-12-03 Hochdruck-Turbinenschaufel mit gekühlter Abströmkante

Country Status (9)

Country Link
US (1) US6830431B2 (es)
EP (1) EP1318274B1 (es)
JP (1) JP4012054B2 (es)
CA (1) CA2412989C (es)
DE (1) DE60201325T2 (es)
ES (1) ES2225740T3 (es)
FR (1) FR2833298B1 (es)
RU (1) RU2297537C2 (es)
UA (1) UA80246C2 (es)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2864990B1 (fr) * 2004-01-14 2008-02-22 Snecma Moteurs Perfectionnements apportes aux fentes d'evacuation de l'air de refroidissement d'aubes de turbine haute-pression
US7503749B2 (en) * 2005-04-01 2009-03-17 General Electric Company Turbine nozzle with trailing edge convection and film cooling
FR2887287B1 (fr) * 2005-06-21 2007-09-21 Snecma Moteurs Sa Circuits de refroidissement pour aube mobile de turbomachine
KR100847523B1 (ko) * 2006-12-29 2008-07-22 엘지전자 주식회사 터보팬
US8002525B2 (en) * 2007-11-16 2011-08-23 Siemens Energy, Inc. Turbine airfoil cooling system with recessed trailing edge cooling slot
FR2924156B1 (fr) * 2007-11-26 2014-02-14 Snecma Aube de turbomachine
US8157504B2 (en) * 2009-04-17 2012-04-17 General Electric Company Rotor blades for turbine engines
FR2954798B1 (fr) 2009-12-31 2012-03-30 Snecma Aube a ventilation interieure
US8608429B2 (en) * 2010-05-28 2013-12-17 General Electric Company System and method for enhanced turbine wake mixing via fluidic-generated vortices
US10107108B2 (en) 2015-04-29 2018-10-23 General Electric Company Rotor blade having a flared tip
DE102020207646A1 (de) * 2020-06-22 2021-12-23 Siemens Aktiengesellschaft Turbinenschaufel und Verfahren zum Bearbeiten einer solchen

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE794195A (fr) * 1972-01-18 1973-07-18 Bbc Sulzer Turbomaschinen Aube directrice refroidie pour des turbines a gaz
GB2121483B (en) * 1982-06-08 1985-02-13 Rolls Royce Cooled turbine blade for a gas turbine engine
US4601638A (en) * 1984-12-21 1986-07-22 United Technologies Corporation Airfoil trailing edge cooling arrangement
US5403158A (en) * 1993-12-23 1995-04-04 United Technologies Corporation Aerodynamic tip sealing for rotor blades
WO1998000627A1 (en) * 1996-06-28 1998-01-08 United Technologies Corporation Coolable airfoil for a gas turbine engine
CA2334071C (en) * 2000-02-23 2005-05-24 Mitsubishi Heavy Industries, Ltd. Gas turbine moving blade

Also Published As

Publication number Publication date
JP2003193804A (ja) 2003-07-09
CA2412989A1 (fr) 2003-06-05
EP1318274B1 (fr) 2004-09-22
US6830431B2 (en) 2004-12-14
EP1318274A1 (fr) 2003-06-11
RU2297537C2 (ru) 2007-04-20
JP4012054B2 (ja) 2007-11-21
FR2833298B1 (fr) 2004-08-06
DE60201325D1 (de) 2004-10-28
CA2412989C (fr) 2008-09-23
FR2833298A1 (fr) 2003-06-13
US20030108425A1 (en) 2003-06-12
ES2225740T3 (es) 2005-03-16
UA80246C2 (uk) 2007-09-10

Similar Documents

Publication Publication Date Title
DE602004003331T2 (de) Kühlluftauslass-Schlitze von Turbinenschaufeln
EP1267041B1 (de) Gekühlte Turbinenschaufel
DE60018817T2 (de) Gekühlte Gasturbinenschaufel
DE602005000350T2 (de) Turbinenstatorschaufel mit verbesserter Kühlung
DE69718673T2 (de) Kühlbare schaufelstruktur für eine gasturbine
EP0902164B1 (de) Plattformkühlung für Gasturbinen
DE60037926T2 (de) Einrichtung und Methode zum Stabilisieren der Kernströmung in einer Gasturbine
EP1757773B1 (de) Hohle Turbinenschaufel
DE3019920C2 (de) Einrichtung zur äußeren Ummantelung der Laufschaufeln von Axialturbinen für Gasturbinentriebwerke
DE19809008C2 (de) Gasturbinenschaufel
DE102004003354B4 (de) Turbinen-Laufschaufel und Gasturbine
DE60201325T2 (de) Hochdruck-Turbinenschaufel mit gekühlter Abströmkante
DE2717810A1 (de) Gasturbinenlaeufer mit keramischen schaufeln
DE3930324A1 (de) Stromlinienfoermige turbinenschaufel
DE19634238A1 (de) Kühlbare Schaufel
EP2084368B1 (de) Turbinenschaufel
EP3473808B1 (de) Schaufelblatt für eine innengekühlte turbinenlaufschaufel sowie verfahren zur herstellung einer solchen
EP2282014A1 (de) Rinförmiger Strömungskanalabschnitt für eine Turbomaschine
WO2003054356A1 (de) Thermisch belastetes bauteil
DE602004002004T2 (de) Mit verringertem Kühlluftdurchstrom gekühlte Turbinenschaufel
DE602004010557T2 (de) Ringförmige Leitschaufelplattform einer Niederdruckstufe einer Gasturbine
EP1675702B1 (de) Gasturbine und laufschaufel für eine strömungsmaschine
EP1510653B1 (de) Gekühlte Turbinenschaufel
DE3122484A1 (de) Laufschaufel
EP2860356A1 (de) Strömungsmaschine

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: CBDL PATENTANWAELTE, 47051 DUISBURG

8327 Change in the person/name/address of the patent owner

Owner name: SNECMA, PARIS, FR